EP 1773660 A1 20070418 - AIRCRAFT ENGINE UNIT
Title (en)
AIRCRAFT ENGINE UNIT
Title (de)
FLUGZEUGMOTOREINHEIT
Title (fr)
ENSEMBLE MOTEUR POUR AERONEF
Publication
Application
Priority
- FR 2005050637 W 20050801
- FR 0451784 A 20040804
Abstract (en)
[origin: US7624945B2] The invention relates to an engine assembly for an aircraft comprising a turbojet, a engine mount pylon, and a plurality of engine mounts inserted between the engine mount pylon and the turbojet. According to the invention, the plurality of engine mounts comprises a engine mount (6a) designed so as to uniquely resist forces applied along a direction (Y) transverse to the turbojet, this engine mount (6a) comprising an intermediate fitting (46) assembled onto a first fitting (40) fixed to the pylon through two swivel axes (48) oriented parallel along a vertical direction (Z), and a pin (56) oriented along a longitudinal direction (X) and fixed to the intermediate fitting, the pin being installed on a second fitting (58) fixed to the turbojet, with clearance along the longitudinal direction (X).
IPC 8 full level
B64D 27/26 (2006.01)
CPC (source: EP US)
B64D 27/40 (2024.01 - EP US); B64D 27/402 (2024.01 - EP); B64D 27/402 (2024.01 - US)
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
FR 2873985 A1 20060210; FR 2873985 B1 20061124; AT E416975 T1 20081215; BR PI0513867 A 20080520; CA 2576518 A1 20060302; CA 2576518 C 20140225; CN 1993268 A 20070704; CN 1993268 B 20110615; DE 602005011633 D1 20090122; EP 1773660 A1 20070418; EP 1773660 B1 20081210; JP 2008509318 A 20080327; JP 4676982 B2 20110427; RU 2007107929 A 20080910; RU 2381149 C2 20100210; US 2007228213 A1 20071004; US 7624945 B2 20091201; WO 2006021721 A1 20060302
DOCDB simple family (application)
FR 0451784 A 20040804; AT 05797577 T 20050801; BR PI0513867 A 20050801; CA 2576518 A 20050801; CN 200580026317 A 20050801; DE 602005011633 T 20050801; EP 05797577 A 20050801; FR 2005050637 W 20050801; JP 2007524380 A 20050801; RU 2007107929 A 20050801; US 57166605 A 20050801